Three-dimensional temperature gradient mechanism in selective laser melting of Ti-6Al-4V
Selective laser melting (SLM) is widely used in making three-dimensional functional parts
layer by layer. Temperature magnitude and history during SLM directly determine the molten …
layer by layer. Temperature magnitude and history during SLM directly determine the molten …
The actuator surface model: a new Navier–Stokes based model for rotor computations
WZ Shen, JH Zhang, JN Sørensen - 2009 - asmedigitalcollection.asme.org
This paper presents a new numerical technique for simulating two-dimensional wind turbine
flow. The method, denoted as the 2D actuator surface technique, consists of a two …
flow. The method, denoted as the 2D actuator surface technique, consists of a two …
Impact of Unsteady Wakes on the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade
The aerodynamics of a high-speed low-pressure turbine (LPT) cascade were investigated
under steady and unsteady inlet flows. The tests were performed at outlet Mach (M) and …
under steady and unsteady inlet flows. The tests were performed at outlet Mach (M) and …
Endwall loss in turbine cascades
JD Coull - Journal of Turbomachinery, 2017 - asmedigitalcollection.asme.org
Prior to the detailed design of components, turbomachinery engineers must guide a mean-
line or throughflow design toward an optimum configuration. This process requires a …
line or throughflow design toward an optimum configuration. This process requires a …
An experimental test case for transonic low-pressure turbines-part 2: Cascade aerodynamics at on-and off-design reynolds and mach numbers
G Lopes, L Simonassi… - … Expo: Power for …, 2022 - asmedigitalcollection.asme.org
In this two-part paper, a novel test-case for transonic low-pressure turbines (LPT) is
presented. The current study is a comprehensive report on the design, commissioning and …
presented. The current study is a comprehensive report on the design, commissioning and …
Large eddy simulation and RANS analysis of the end-wall flow in a linear low-pressure-turbine cascade—Part II: loss generation
In low-pressure turbines (LPT) at design point, around 60–70% of losses are generated in
the blade boundary layers far from end walls, while the remaining 30–40% is controlled by …
the blade boundary layers far from end walls, while the remaining 30–40% is controlled by …
Secondary flows and loss caused by blade row interaction in a turbine stage
G Pullan - 2006 - asmedigitalcollection.asme.org
A study of the three-dimensional stator-rotor interaction in a turbine stage is presented.
Experimental data reveal vortices downstream of the rotor which are stationary in the …
Experimental data reveal vortices downstream of the rotor which are stationary in the …
Improving the performance of a turbine with low aspect ratio stators by aft-loading
G Pullan, J Denton, E Curtis - 2006 - asmedigitalcollection.asme.org
Experimental data and numerical simulations are presented from a research turbine with low
aspect ratio nozzle guide vanes (NGVs). The combined effects of mechanical and …
aspect ratio nozzle guide vanes (NGVs). The combined effects of mechanical and …
The effect of clearance on shrouded and unshrouded turbines at two levels of reaction
S Yoon, E Curtis, J Denton… - Journal of …, 2014 - asmedigitalcollection.asme.org
In this paper, the effect of seal clearance on the efficiency of a turbine with a shrouded rotor
is compared with the effect of the tip clearance when the same turbine has an unshrouded …
is compared with the effect of the tip clearance when the same turbine has an unshrouded …
The influence of blade tip gap variation on the flow through an aggressive S-shaped intermediate turbine duct downstream a transonic turbine stage: part II—time …
E Go¨ ttlich, A Marn, R Pecnik… - … Expo: Power for …, 2007 - asmedigitalcollection.asme.org
The demand of further increased bypass ratio of aero engines will lead to low pressure
turbines with larger diameters rotating at lower speed. Therefore it is necessary to guide the …
turbines with larger diameters rotating at lower speed. Therefore it is necessary to guide the …